strake

英

美

网络  边条翼; 边条; 列板; 板列; 防滑轮爪

第三人称单数：strakes　过去分词：straked　复数：strakes　

COCA.33341

英英释义

noun

• thick plank forming a ridge along the side of a wooden ship
  Synonym:wale

双语例句

• Using strake vortex to reduce the distortion of a Y shaped inlet
  利用边条涡抑制Y形进气道流场畸变
• Some unusual control surfaces such as spoiler, clam-shell aileron, body-nose strake, movable wing-tip are investigated on two typical configurations.
  在两种典型布局上研究了扰流板、开裂副翼、机头边条、活动和偏转翼梢及舵面的方向控制特性。
• Experiments show that the adaptability of the self-organized fuzzy controller works very well in different work condition, and can realize variable cushioning strake.
  实验结果表明，自组织模糊控制器对不同的工况有较强的适应性，并实现了可变的缓冲行程。
• Some measures improving the longitudinal and lateral stabilities of combat aircraft with strake wing configuration are discussed.
  对边条机翼布局战斗机的纵、横向稳定性改进措施进行了研究。
• The fixed strake and strake flap will also improve the lift-drag characteristics at medium angles-of-attack, the hinged strake and strake flap will raise the stall behavior.
  固定边条和边条襟翼还可改善中小迎角的升阻性能，链接边条和边条襟翼则可使失速性能提高。
• This paper gives a review on the technical development of spar platform, including the research on dynamic response, mooring system, fatigue and coupled analysis and the design of heave plate and strake configuration.
  本文介绍Spar平台的发展趋势及其关键技术的研究，包括平台动力响应、系泊系统、疲劳分析、耦合分析以及垂荡板和侧板的设计研究。
• Research on the Low Speed Aerodynamic Characteristics of an Aircraft with a Small Strake and Controlling Separation at the Outer Part of Its Wing
  一种小边条飞机的低速气动特性及其外翼分离控制研究
• The valve is driven directly by a large strake multilayer piezoelectric stack, its displacement actuates the power cascade spool after amplification by a lever mechanism.
  该阀采用大行程的压电叠堆作为驱动元件，经杠杆放大后的位移直接驱动功率级滑阀。
• The maximum lift coefficient could be raised by30%. It has been shown that moving surface is an excellent technique to control separated flow over the strake wing.
  结果表明，在这种机翼上转动前缘对控制分离是有效的，升力增量最大可达30%。
• Lateral-Direction Aerodynamic Characteristics and Forebody Strake Control of an Aircraft Undergoing Pitching Oscillation on High Attack Angle
  飞机大迎角俯仰运动下的横侧向气动特性及被动控制